ADL110 Installation Manual
Contents
1. ADL110 Installation Manual Version 0 94 12 02 2013 ADL110 Installation Manual 1 15 Revision 0 94 12 02 2013 Contents I Version tee EE 3 2x PAGE E 3 Se TEE RR e re EE 3 4 gt Gertificationr ADETI O s Sees 3 5 EE EE ne een see 3 6 Warning see ee ee 3 T Emergency PIOCCUUIGS a ss 4 GB YDIMENSIONE e IAA 4 We CEET EE 6 e IMMA Tee GE 6 Ce te Ei E TEE EEN 6 9 2 1 Glareshield antenna installation 6 9 2 2 External antenna installation 7 9 2 3 Antennartesingns ass ra aA ANAL AI 7 9 3 Panel cutout nenne 7 9 3 1 Re e E EE 7 9 4 Adapter Mount eesesieeebesieegbeieegbe eege eg Ee Aeegbe kee Seege eege eegen 8 9 55 AWNING RE 10 9 5 1 Voltage Connechor nennen 10 9 5 2 Antenna Connector EE 10 9 5 3 Aviation data WME ACE esse ee 11 9 5 4 Firmware Update mtertace i 11 lW lt Gooling c he girone ces la aaa 12 11 Post installation checkout 12 i Documentatii Ni Need 13 13 Continued MAINTENANCE nennen 13 14 Software and database updates 13 19 1roubleshoalngs sense ara 13 16 Specifications ADL110 EE 13 17 Part number reference cc ceccccecsseccceceeseeeecceeseeeeceeeseeeeeeeeseeseeeeeeeeeetenseeeeees 14 ET EE 15 ADL110 Installation Manual 2 15 Revision 0 94 12 02 2013 1 Version History Version 0 9 published 10 12 2012 Version 0 91 published 21 01 2013 Version 0 92 published 02 02 2013 Version 0 93 published 09 02 2013 Version 0 94 publ2. ation Manual 14 15 Revision 0 94 12 02 2013 18 Contact Ingenieurb ro Dr Golze Bredowstr 29 10551 Berlin http www ing golze de adl110 ing golze de 49 30 39805204 ADL110 Installation Manual 15 15 Revision 0 94 12 02 2013
3. connect ADL110 ADL110 Update Port GPS Reminder Only connect the pins described above Connecting additional pins may damage the equipment 10 Cooling Generally the ADL110 does not require any means of active cooling If mounted in a position where the specified temperature limit might by exceeded additional air should be implemented 11 Postinstallation checkout Disconnect the power connector Turn on the aircraft electrical system and measure the voltage at the connector is within specification Turn the aircraft power system off and reinstall power connector Verify the wiring is secure and has no interference with any other electrical or mechanical system Especially make sure the wiring is free of any flight control systems ADL110 Installation Manual 12 15 Revision 0 94 12 02 2013 Turn the aircraft electrical system on and verify the ADL110 is running Place the aircraft in a position with good panoramic view to the sky Verify the device has got Iridium and GPS reception using the blue signal bars on the right top side of the screen The left bars indicate iridium signal quality and the right bar indicates GPS signal quality If the GPS has not been running recently it may require several minutes to get a fix The Iridium system will usually get a satellite fix much faster In order to start an Iridium transmission the software will require a minimum of two Iridium signal quality bars as experience has shown that b
4. cturer use do not connect 9 Manufacturer use do not connect 10 Manufacturer use do not connect 11 Manufacturer use do not connect 12 Manufacturer use do not connect 13 Manufacturer use do not connect 14 Manufacturer use do not connect 15 Manufacturer use do not connect Table 1 15pin D SUB pin description Please consult the installation manual of your FMS GPS for the required pin configuration Please not that usually the Garmin 430 530 devices will only be able to supply aviation out data on one RS232 port at a time Therefore if you have multiple devices requiring the aviation data you will probably have to physically connect them to the same pin 9 5 4 Firmware Update interface The internal firmware can be updated by the user or installer For the detailed procedure please refer to the current user manual While this update can be done with the ADL110 outside the aircraft we recommend the installation of an additional 15 pin D SUB connector for updates We provide a pre wired setup which corresponds to figure 12 Please not that the ADL110 update plug must be installed when the device is running As figure 12 shows if not installed aviation data input will not work ADL110 Installation Manual 11 15 Revision 0 94 12 02 2013 Aviation Data ADL110 ADL110 ADL110 Update Update 1 GND Plug D SUB D SUB 15 pin 2 RS232 OUT 15 pin D SUB male male 15 pin 3 RS232 IN Ee 7 Update Pin Figure 12 Inter
5. elow this level transmissions may become unreliable Do a test run and download a METAR for an airport for example EDDB Please note A test transmission will only be possible if at the time of installation the Iridium data contract for the device has already been activated Verify the rest of the avionics system in order to assure that no other systems have malfunctions after the installation 12 Documentation Produce detailed installation documentation Join this documentation including this manual to the aircraft records Join the current ADL110 user manual to the pilots operation manual 13 Continued maintenance No regular maintenance is required 14 Software and database updates Please contact us for information on software and database updates 15 Troubleshooting Verify all connectors and proper power supply Inspect the device for visible damage The device does not contain any field serviceable parts It the device is believed to be defunct please contact us for repair 16 Specifications ADL110 Voltage 7 to 30V Circuit breaker 1A Internal fuse 2A Maximum consumption 6W Temperature range operation 20 to 70 C Temperature range storage 30 to 70 C Weight excl installation material 480g ADL110 Installation Manual 13 15 Revision 0 94 12 02 2013 17 Part number reference Partnumber Description ADL110 Weather display RNG043 Mounting adapter ADP035 Mounting adapter ADL110 Install
6. ined to the standards of certified aviation databases ADL110 Installation Manual 3 15 Revision 0 94 12 02 2013 7 Emergency procedures If you suspect any malfunction of the ADL110 or interference with other aircraft systems deactivate the device by pulling deactivating the aircraft circuit breaker for the device Do not reactivate the device until the problem has been investigated and resolved on the ground In case of a generator failure or similar situation requiring electric load shedding deactivate the ADL110 by pulling deactivating the aircraft circuit breaker for the device 8 Dimensions Figures 1 and 2 show the outside dimensions of the ADL110 enclosure excluding the rear connectors Please refer to the section Panel cutout for depth requirements Figures 3 and 4 show pictures of the enclosure 85 0 mm Leg 85 0 mm Figure 1 Front dimensions of housing ADL110 Installation Manual 4 15 Revision 0 94 12 02 2013 85 0mm 75 0mm Figure 2 Side dimensions of housing Figure 3 Enclosure front view ADL110 Installation Manual 5 15 Revision 0 94 12 02 2013 Figure 4 Enclosure rear view 9 Installation 9 1 Inspection Inspect the ADL110 and all supplied parts for condition and completeness Verify on our website that you have the most up to date version of this installation manual 9 2 Iridium Antenna The device uses an Iridium antenna to communicate with the Iridium satellite netwo
7. ired Please note that the ADL110 does not provide any lightning protection When using an external antenna the antenna must be grounded and provide full certified lightning protection 9 2 3 Antenna testing Please note that the Iridium network requires a better view to the sky than the GPS receiver Therefore make sure the antenna is placed properly and when testing do not place the aircraft nextto a big hangar or similar objects obstructing the sky 9 3 Panel cutout diameter of the enclosure is 3 Inch 76 2mm Therefore a minimum cutout diameter of 78mm is required The device itself has got a depth of 76 mm behind the panel front plate In order to allow a proper installation of connectors an installation space with a minimum depth of 130 mm behind the panel front should be selected If this is not possible small connectors can be used If you plan such an installation please contact us 9 3 1 Direct Mount In this case the device is attached to the panel using four M3 screws Figure 6 shows the required cutout We recommend using our aluminum ring part number RNG043 in order to provide threads for these screws Figure 7 depicts the RNG043 adapter ADL110 Installation Manual 7 15 Revision 0 94 12 02 2013 A 4 holes 3mm 77 7mm Minimum cutout 78mm O O Figure 6 Panel cutout for direct mount Figure 7 The rear ring providing M3 threads for direct mount partnumber RNG043 9 4 Adapter mount As an alternat
8. ished 12 02 2013 2 Page Index This manual contains numbered pages 1 to 15 3 General Description The ADL110 is a flight data link device It allows downloading weather data while in flight Besides it features in flight SMS communication The data link works through the Iridium satellite network with global coverage 4 Certification ADL110 The ADL110 can be installed in certified aircraft if a suitable minor change is used The device itself does not come with any certification Please consult the minor change documentation for details 5 Disclaimer The ADL110 is provided as a non certified component The only basis on witch it can be installed is an appropriate minor change It is the sole responsibility of the user and installer that is installed and used in a legal way The device may stop working at any time Do not undertake flights you would not undertake without the ADL110 6 Warning While we do everything we can to ensure quality the ADL110 devices might not work at any time In addition they may display false information Never penetrate weather based on the information provided by the ADL110 This information is for situational awareness only The device features a GPS moving map system This system is designed to display the aircraft position in relation to the weather data It is not designed as a means of primary navigation Especially the build in database is not updated in a regular aviation cycle It is also not mainta
9. ive to the direct mount option the device can also be mounted using our ADP035 adapter This way a more common 3 1 2 inch dilling scheme can be used The required panel cutout is depicted as figure 8 ADL110 Installation Manual 8 15 Revision 0 94 12 02 2013 62 86mmm ea 4 holes 3mm O 62 86mm Minimum cutout 78mm Figure 8 Standard 3 1 8 panel cutout for mount with adapter The adapter ADP035 consists of two parts The square adapter plate is mounted on the front side of the panel and the round ring provides the threads to secure it to the panel using 4 flat heat M3 screws Figure 9 shows the ADP035 adapter Finally with the adapter installed the device can be pushed from the front into the adapter and secure with four flat head M3x10mm screws Pay attention not to damage the threads in the adapter ADL110 Installation Manual 9 15 Revision 0 94 12 02 2013 Figure 9 ADP035 adapter allowing the installation in a standard 3 1 8 panel cutout 9 5 Wiring 9 5 1 Voltage connector The device must be connected to the electrical power distribution system of the aircraft The connector on the device backside is a MIL C 5015 10SL3S figure 10 An appropriate matching connector on the aircraft side is MIL C 5015 10SL3 using an appropriate strain relief figure 11 The connector is allocated as follows Pin A Vcc 10V 30V DC Pin B Gnd Pin C Unused The device will accept DC 7V to 30V We recommend installi
10. ng a 1A circuit breaker in line with the ADL110 For additional protection the device has got an internal fuse rated at 2A The maximum power consumption will be 6W Figure 10 MIL C 5015 10SL3S connector of the device Figure 11 MIL C 5015 10SL3 and strain relief 9 5 2 Antenna connector The device features a rear BNC male connector Connect the antenna by twisting the BNC female connector of the antenna onto the device connector ADL110 Installation Manual 10 15 Revision 0 94 12 02 2013 9 5 3 Aviation data interface The 15 pin male D SUB connector on the backside of the enclosure provides the optional possibility to interconnect the ADL110 with a FMS GPS navigator transmitting the current route flightplan information via RS232 to the device This communication is one way only The ADL110 will only act as a receiver The supported data format is the Aviation data format The device has been tested with the Garmin 530 430 series devices If you wish to connect other flightplan sources please contact us Please not the Aviation In feature when connected must be activated in the software on the FPL page using the right side button FPL IN ADL110 15pin D Function SUB pin 1 GND 2 RS232 OUT 3 RS232 IN Aviation data input 4 Manufacturer use do not connect 5 Manufacturer use do not connect 6 Manufacturer use do not connect 7 Update Pin 8 Manufa
11. rk This antenna is also used by the build in GPS receiver If an outside mounted Iridium antenna is available this will represent the best solution If such an antenna is not available we recommend using an antenna mounted on the instrument glareshield This will provide good reception at a much lower cost than an outside antenna installation The antenna will be connected to the device using a BNC female connector If your antenna does not come with such a connecter it must be crimped on the cable 9 2 1 Glareshield antenna installation In the case of a glareshield installation we recommend the Iridium SYN7391 C antenna This antenna has been tested with good results and the antenna does not incorporate any magnetic mount which could deviate the magnetic compass In general you should try to place the antenna as far forward as possible in order to give it the best panoramic opening to the sky possible Figure 5 shows such a glareshield installation of the SYN7391 C antenna ADL110 Installation Manual 6 15 Revision 0 94 12 02 2013 Figure 5 Iridium SYN7391 C antenna on glareshield 9 2 2 External antenna installation We recommend the use of the S67 1575 109 antenna manufactured by Sensor Systems Inc Before attempting the installation of any outside antenna and drilling any holes in the hull please make sure you have the required documentation and certification For any certified aircraft a minor or even a major change will be requ
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